Flight Instruments: A51A9026-1, A51A9026-3, A51A9129-13
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| A51A9026-1 A51A90261 | 6610-00-172-6959 | Indicator, Position | Width: 1.437 inches nominal Electrical Connection Quantity: 1 Height: 3.750 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9026-11 A51A902611 | 6610-00-239-8611 | Transmitter, Failure | Northrop Grumman Systems Corporation (26512) | ||
| A51A9026-13 A51A902613 | 6610-00-239-8612 | Transmitter, Failure | III End Item Identification: Aircraft, tomcat F-14 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9026-15 A51A902615 | 6610-00-172-6978 | Transmitter, Wing Sw | Special Features: 30 degree pressure angle; teeth - Qty 8; pitch dia 0.1667 inch | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9026-17 A51A902617 | 6610-00-029-9407 | Transmitter, Wing Sweep | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9026-19 A51A902619 | 6610-01-384-1462 | Indicator, Position | Special Features: Transmitter, indictor set, wing sweep A/A37J-6 End Item Identification: Aircraft model F-14D Reference Number Differentiating Characteristics: As differeniated by source control drawing | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9026-3 A51A90263 | 6610-00-172-6979 | Transmitter, Wing Sweep | III End Item Identification: F-14 tomcat | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9026-7 A51A90267 | 6610-00-172-6981 | Transmitter, Failure | Special Features: As modified by source controlling dwgfmsc 26512 no. A51A9026&7 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9026-9 A51A90269 | 6610-00-172-6982 | Transmitter, Failure | III End Item Identification: Aircraft, tomcat F-14 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9027-3 A51A90273 | 6610-00-155-4705 | Indicator, Angle | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9027-5 A51A90275 | 6610-00-110-3624 | Indicator, Angle | Width: 1.437 inches nominal Mounting Facility Type and Quantity: 2 screw Electrical Connection Quantity: 1 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9051-1 A51A90511 | 6610-00-001-1792 | Indicator, Instrument Landing, Air | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9055-1 A51A90551 | 6610-00-558-0399 | Indicator, Turn and Slip | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9075-11 A51A907511 | 6610-00-466-9991 | Computer, Air Data | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9075-13 A51A907513 | 6610-00-466-9990 | Computer, Air Data | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9075-15 A51A907515 | 6610-00-466-9987 | Computer, Air Data | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9075-17 A51A907517 | 6610-01-019-9233 | Computer, Air Data | Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. Power Source: External Intelligence Input Method: Electrical | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9075-9 A51A90759 | 6610-00-327-4274 | Computer, Air Data | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9129-11 A51A912911 | 6610-00-140-1487 | Programmer, Air Inle | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9129-13 A51A912913 | 6610-01-010-7094 | Programmer, Air Inlet Control | Northrop Grumman Systems Corporation (26512,61174) |